CN112299883A - High-temperature-resistant protective coating of silicon carbide heating element and preparation method thereof - Google Patents

High-temperature-resistant protective coating of silicon carbide heating element and preparation method thereof Download PDF

Info

Publication number
CN112299883A
CN112299883A CN201910680290.1A CN201910680290A CN112299883A CN 112299883 A CN112299883 A CN 112299883A CN 201910680290 A CN201910680290 A CN 201910680290A CN 112299883 A CN112299883 A CN 112299883A
Authority
CN
China
Prior art keywords
silicon carbide
heating element
sic
coating
resistant protective
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201910680290.1A
Other languages
Chinese (zh)
Other versions
CN112299883B (en
Inventor
秦长勇
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Vivotech Instruments Yangzhou Co ltd
Original Assignee
Vivotech Instruments Yangzhou Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Vivotech Instruments Yangzhou Co ltd filed Critical Vivotech Instruments Yangzhou Co ltd
Priority to CN201910680290.1A priority Critical patent/CN112299883B/en
Publication of CN112299883A publication Critical patent/CN112299883A/en
Application granted granted Critical
Publication of CN112299883B publication Critical patent/CN112299883B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/80After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
    • C04B41/81Coating or impregnation
    • C04B41/85Coating or impregnation with inorganic materials
    • C04B41/87Ceramics
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/009After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B41/00After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
    • C04B41/45Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
    • C04B41/50Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements with inorganic materials
    • C04B41/5024Silicates

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Materials Engineering (AREA)
  • Structural Engineering (AREA)
  • Organic Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • Ceramic Products (AREA)

Abstract

The invention discloses a high-temperature-resistant protective coating of a silicon carbide heating element and a preparation method thereof, belonging to the technical field of preparation of high-temperature-resistant protective coatings2) And an in-situ sintering reaction of the coated slurry with titanium oxide (TiO)2) And zirconium oxide (ZrO)2) Or Yttria Stabilized Zirconia (YSZ) ceramic powder as a raw material. The high-temperature resistant protective coating of the silicon carbide heating element and the preparation method thereof provided by the invention take titanium oxide and zirconia or Yttria Stabilized Zirconia (YSZ) ceramic powder as raw materials, and a compact ceramic protective layer of silicon Zirconium Titanium Silicate (ZTS) is formed by ball milling pulping, coating and high-temperature sintering reaction, so that the oxidation resistance and corrosion resistance of the silicon carbide (SiC) heating element can be greatly improved, the process is simple, the cost is low, and the high-temperature resistant protective coating is suitable for large-scale industrial use.

Description

High-temperature-resistant protective coating of silicon carbide heating element and preparation method thereof
Technical Field
The invention relates to the technical field of preparation of high-temperature-resistant protective coatings, in particular to a high-temperature-resistant protective coating of a silicon carbide heating element and a preparation method thereof.
Background
Silicon carbide (SiC) ceramic materials have many excellent material properties, and are widely used in the fields of petroleum, chemical engineering, microelectronics, automobiles, aerospace, heavy machinery, atomic energy and the like, for example, silicon carbide ceramics are widely used in parts such as precision bearings and the like by utilizing the advantages of wear resistance, large elastic modulus, corrosion resistance and the like of the silicon carbide ceramic materials; the silicon carbide ceramic is widely applied to grinding in the field of machining by utilizing the advantages of wear resistance, high hardness and the like of the silicon carbide ceramic material; the silicon carbide ceramic material is widely applied to industrial high-temperature heating elements by utilizing the advantages of excellent electrical conductivity, high-temperature thermal stability and the like of the silicon carbide ceramic material, and various shapes can be prepared to meet the requirement of industry due to the good forming characteristic of the silicon carbide ceramic materialThe field multi-working condition use requirements; silicon carbide ceramic materials are also widely used in military equipment, protective layers for bulletproof armored vehicles, and the like. In a plurality of application fields of silicon carbide ceramic materials, the silicon carbide ceramic material is used as an industrial high-temperature heating element and is an important application. Under a certain working condition temperature, a layer of silicon dioxide (SiO) can be formed on the surface of the silicon carbide ceramic material through oxidation2) The silicon dioxide layer has certain oxidation resistance; when the working condition temperature is higher than 800 ℃, the silicon dioxide layer can form a porous structure to generate embrittlement and easily generate associated chemical reaction, so that the antioxidant protection effect is reduced or even lost; when the working condition temperature is higher than 1650 ℃, the silicon carbide (SiC) is converted from passive oxidation to active oxidation under the aerobic condition, which can cause the heating element to be seriously damaged, and particularly, under the severe working condition, the silicon carbide (SiC) ceramic material is easy to react with active gas, which causes oxidation and corrosion, and reduces or even loses the conductivity, thereby limiting the application of the silicon carbide (SiC) ceramic material under the high-temperature severe working condition. At present, no effective technical measures are available for processing the technical current situation that the conductivity of a silicon carbide (SiC) ceramic material is reduced or even lost due to passive oxidation and corrosion under severe working conditions. Therefore, a high temperature resistant protective coating of a silicon carbide heating element with simple process, low cost and stable performance and a preparation method thereof are needed.
Summary of the invention
The invention aims to solve the problem that a silicon carbide (SiC) ceramic material is easy to react with active gas under severe working conditions to cause oxidation and corrosion and reduce or even lose conductivity under the existing severe working conditions, and provides a high-temperature resistant protective coating of a silicon carbide heating element, which has the advantages of simple process, low cost and stable performance, and a preparation method thereof.
In order to achieve the purpose, the invention is realized by the following technical scheme:
a high-temperature resistant protective coating for silicon carbide (SiC) heating elements, the coating being formed by pre-oxidizing silicon dioxide (SiO) on the surface of the silicon carbide (SiC) heating element2) And the coated slurry is subjected to in-situ sintering reactionThe slurry is made of titanium oxide (TiO)2) And zirconium oxide (ZrO)2) Or Yttria Stabilized Zirconia (YSZ) ceramic powder as a raw material.
A preparation method of a high-temperature resistant protective coating of a silicon carbide (SiC) heating element comprises the following steps:
step 1: silicon carbide (SiC) heating element pretreatment
Cleaning the surface of a silicon carbide (SiC) heating element, putting the silicon carbide (SiC) heating element into an oven to be dried for 2 hours at the temperature of 150 ℃, and then putting the silicon carbide (SiC) heating element into a high-temperature furnace to be heated for 2 to 5 hours at the temperature of 1000 ℃ in the air or oxygen atmosphere to form a white silicon oxide layer on the surface;
step 2: preparation of coating slurries
Weighing 50-60 g of titanium oxide (TiO)2) And 40 to 50g of zirconium oxide (ZrO)2) Or adding yttria-stabilized zirconia (YSZ) ceramic powder into a zirconia ceramic ball-milling tank with the volume of 500-1000 mL, adding 200-400 mL of grinding balls, 250-500 mL of purified water and 10-20 g of PVB adhesive into the zirconia ceramic ball-milling tank, sealing and filling the mixture into a planetary ball mill, operating at 500RPM for 24 hours, and filtering to remove zirconium balls to form 250-500 mL of slurry with the solid content of 40%;
and step 3: preparation of the coating
Uniformly coating the slurry formed in the step 2 on the silicon oxide layer formed in the step 1 by adopting a brush coating mode, wherein the coating thickness is 100-150 mu m, and naturally airing for 4 hours or heating and drying for 2 hours at 150 ℃;
and 4, step 4: in-situ sintering of coatings
And (3) placing the silicon carbide (SiC) heating element coated with the coating formed in the step (3) into a high-temperature sintering furnace, heating to 1200-1400 ℃ at the heating rate of 10-15 ℃/min, and preserving heat for 1-2 hours to generate a Zirconium Titanium Silicate (ZTS) protective layer on the surface.
In the above method for preparing the high temperature resistant protective coating of the silicon carbide (SiC) heating element, in the step 2, zirconium oxide (ZrO) is used2) The purity is more than or equal to 99.5 percent.
In the step 2, the yttria-stabilized zirconia ceramic powder is added to the high temperature resistant protective coating of the silicon carbide (SiC) heating elementY of (A) is2O3The content is 3-5%.
In the step 2, the ratio of the grinding balls to the grinding balls is D10: D6: D4: 2:5: 3.
In the above preparation method of the high temperature resistant protective coating for the silicon carbide (SiC) heating element, in the step 2, the PVB content of the PVB binder is 3-6W%.
Compared with the prior art, the invention has the following beneficial effects:
1. the high-temperature resistant protective coating of the silicon carbide heating element provided by the invention takes titanium oxide and zirconium oxide or Yttria Stabilized Zirconia (YSZ) ceramic powder as raw materials, and a compact ceramic protective layer of silicon Zirconium Titanium Silicate (ZTS) is formed by ball milling pulping, coating and high-temperature sintering reaction, so that the oxidation resistance and corrosion resistance of the silicon carbide (SiC) heating element can be greatly improved, the process is simple, the cost is low, and the high-temperature resistant protective coating is suitable for large-scale industrial use;
2. the invention provides a high-temperature resistant protective coating of a silicon carbide heating element and a preparation method thereof, wherein the surface of the silicon carbide (SiC) heating element is pre-oxidized to form porous silicon dioxide (SiO)2) Filling gaps with ultrafine particles of titanium oxide and zirconium oxide or Yttria Stabilized Zirconia (YSZ) ceramic powder, and sintering at high temperature in situ to form a compact ceramic protective layer of Zirconium Titanium Silicate (ZTS), so that gas is completely prevented from diffusing to a silicon carbide (SiC) surface layer, the silicon carbide protective layer is not easy to fall off, the performance is stable, embrittlement and associated chemical reactions are effectively reduced, and the antioxidant protection effect is improved;
3. compared with the existing preparation methods (such as plasma spraying, sputtering, chemical vapor deposition and the like), the high-temperature-resistant protective coating of the silicon carbide heating element and the preparation method thereof have the advantages of simple process flow, no need of special equipment, low cost and wide market application value.
Drawings
FIG. 1 is a flow chart of the process principle of the present invention.
Detailed Description
In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the following detailed description is combined with the embodiments of the invention: the present embodiment is implemented on the premise of the technical solution of the present invention, and a detailed implementation manner and a process are given, but the scope of the present invention is not limited to the following embodiments.
The invention is further described below with reference to the accompanying drawings:
referring to FIG. 1, a refractory protective coating for a silicon carbide (SiC) heating element is provided, the coating comprising silicon dioxide (SiO) pre-oxidized on the surface of the silicon carbide (SiC) heating element2) And an in-situ sintering reaction of the coated slurry with titanium oxide (TiO)2) And zirconium oxide (ZrO)2) Or Yttria Stabilized Zirconia (YSZ) ceramic powder as a raw material.
A preparation method of a high-temperature resistant protective coating of a silicon carbide (SiC) heating element comprises the following steps:
step 1: silicon carbide (SiC) heating element pretreatment
Cleaning the surface of a silicon carbide (SiC) heating element, putting the silicon carbide (SiC) heating element into an oven to be dried for 2 hours at the temperature of 150 ℃, and then putting the silicon carbide (SiC) heating element into a high-temperature furnace to be heated for 2 to 5 hours at the temperature of 1000 ℃ in the air or oxygen atmosphere to form a white silicon oxide layer on the surface;
step 2: preparation of coating slurries
Weighing 50-60 g of titanium oxide (TiO)2) 40 to 50g of zirconium oxide (ZrO)2) Or adding yttria-stabilized zirconia (YSZ) ceramic powder, 200-400 mL of grinding balls, 250-500 mL of purified water and 10-20 g of PVB adhesive into a zirconia ceramic ball milling tank with the volume of 500-1000 mL, sealing and filling the zirconia ceramic ball milling tank into a planetary ball mill, operating at 500RPM for 24 hours, filtering and removing the zirconium balls to form 250-500 mL of slurry with the solid content of 40%, wherein Y in the yttria-stabilized zirconia (YSZ) ceramic powder2O3The content of the PVB adhesive is 3-5%, the ratio of the grinding balls is D10: D6: D4: 2:5:3, and the content of PVB in the PVB adhesive is 3-6W%;
and step 3: preparation of the coating
Uniformly coating the slurry formed in the step 2 on the silicon oxide layer formed in the step 1 by adopting a brush coating or a coating mode, wherein the coating thickness is 100-150 mu m, and naturally airing for 4 hours or heating and drying for 2 hours at 150 ℃;
and 4, step 4: in-situ sintering of coatings
And (3) placing the silicon carbide (SiC) heating element coated with the coating formed in the step (3) into a high-temperature sintering furnace, heating to 1200-1400 ℃ at a heating rate of 10-15 ℃/min, preserving heat for 1-2 hours, naturally cooling along with the furnace, generating a Zirconium Titanium Silicate (ZTS) protective layer on the surface, adding Yttria Stabilized Zirconia (YSZ) ceramic powder into coating slurry to improve the mechanical property and the thermal expansion property of the protective layer, and adding a PVB adhesive into the coating slurry to facilitate the adjustment of the thickness of the coating and the formation of the coating.
The process principle flow, as shown in the attached figure 1, comprises the following reaction steps:
first, a silicon dioxide (SiO) formed by pre-oxidizing the surface of a silicon carbide (SiC) heating element2) The reaction principle is shown in formula (1),
Figure BDA0002144519700000061
second, silicon dioxide (SiO) formed by pre-oxidizing the surface of the silicon carbide (SiC) heating element2) Titanium oxide (TiO) in layer and coated slurry2) And zirconium oxide (ZrO)2) Reacting, and performing high-temperature in-situ sintering to form a compact Zirconium Titanium Silicate (ZTS) protective layer, wherein the reaction principle is shown in formula (2).
Figure BDA0002144519700000062
Example 1
Step 1, cleaning the surface of a silicon carbide (SiC) heating rod to remove impurities on the surface, and placing the silicon carbide (SiC) heating rod in a high-temperature furnace at 1000 ℃ in an air atmosphere for heating pretreatment for 3 hours to form a white silicon oxide layer on the surface of the silicon carbide (SiC) heating rod.
Step 2, weighing 50g of titanium oxide and 50g of zirconium oxide, wherein the purity of the zirconium oxide is more than or equal to 99.5%, adding the zirconium oxide into a zirconium oxide ceramic ball milling tank with the volume of 500mL, adding grinding balls with the volume of 200mL and the proportion of D10: D6: D4: 2:5:3, adding 250mL of purified water, adding 10g of PVB adhesive, wherein the content of PVB is 3-6W%, sealing and filling the mixture into a planetary ball mill, operating for 24 hours at 500RPM, and filtering to remove the zirconium balls to form 250mL of coating slurry with the solid content of 40%.
And 3, uniformly coating the slurry prepared in the step 2 on the silicon oxide layer formed by pretreating the silicon carbide (SiC) heating rod in the step 1 by adopting a brush coating method or a coating method, wherein the coating thickness is 100 mu m, and naturally airing for 4 hours.
And 4, placing the silicon carbide (SiC) substrate coated in the step 3 into a high-temperature sintering furnace, heating to 1350 ℃ at a heating rate of 10 ℃/min in an air atmosphere for surface sintering, sintering for 1 hour, and naturally cooling along with the furnace.
And (4) taking out the silicon carbide (SiC) heating rod formed in the step (4), and electrifying 220V alternating current to electrically heat the silicon carbide (SiC) heating rod to 1200 ℃ for 72 hours, wherein the surface of the silicon carbide (SiC) heating rod is not oxidized.
Example 2
Step 1, cleaning the surface of a silicon carbide (SiC) heating rod to remove impurities on the surface, and placing the silicon carbide (SiC) heating rod in a high-temperature furnace at 1000 ℃ in an air atmosphere for heating pretreatment for 4 hours to form a white silicon oxide layer on the surface of the silicon carbide (SiC) heating rod.
Step 2, weighing 60g of titanium oxide and 40g of zirconium oxide, wherein the purity of the zirconium oxide is more than or equal to 99.5%, adding the zirconium oxide into a zirconium oxide ceramic ball milling tank with the volume of 500mL, adding grinding balls with the volume of 200mL and the proportion of D10: D6: D4: 2:5:3, adding 250mL of purified water, adding 10g of PVB adhesive, wherein the content of PVB is 3-6W%, sealing and filling the mixture into a planetary ball mill, operating at 500RPM for 24 hours, filtering and removing the zirconium balls to form 250mL of coating slurry with the solid content of 40%.
And 3, uniformly coating the slurry prepared in the step 2 on the silicon oxide layer formed by pretreating the silicon carbide (SiC) heating rod in the step 1 by adopting a brush coating method or a coating method, wherein the coating thickness is 150 mu m, and naturally airing for 4 hours.
And 4, placing the silicon carbide (SiC) substrate coated in the step 3 into a high-temperature sintering furnace, heating to 1350 ℃ at a heating rate of 10 ℃/min in an air atmosphere for surface sintering, sintering for 0.5 hour, and naturally cooling along with the furnace.
And (4) taking out the silicon carbide (SiC) heating rod formed in the step (4), and electrifying 220V alternating current to electrically heat the silicon carbide (SiC) heating rod to 1200 ℃ for 72 hours, wherein the surface of the silicon carbide (SiC) heating rod is not oxidized.
In summary, the basic principles, main features and advantages of the present invention have been shown and described, which are merely examples of the present invention, and are not intended to limit the scope of the present invention. The present invention is not limited to the above-described embodiments, and all equivalent changes and modifications in the shape, structure, characteristics and spirit of the present invention described in the claims should fall within the scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (6)

1. A high temperature resistant protective coating for a silicon carbide (SiC) heating element, the coating comprising silicon dioxide (SiO) pre-oxidized on the surface of the silicon carbide (SiC) heating element2) And an in-situ sintering reaction of the coated slurry with titanium oxide (TiO)2) And zirconium oxide (ZrO)2) Or Yttria Stabilized Zirconia (YSZ) ceramic powder as a raw material.
2. A preparation method of a high-temperature resistant protective coating of a silicon carbide (SiC) heating element is characterized by comprising the following steps:
step 1: silicon carbide (SiC) heating element pretreatment
Cleaning the surface of a silicon carbide (SiC) heating element, putting the silicon carbide (SiC) heating element into an oven to be dried for 2 hours at the temperature of 150 ℃, and then putting the silicon carbide (SiC) heating element into a high-temperature furnace to be heated for 2 to 5 hours at the temperature of 1000 ℃ in the air or oxygen atmosphere to form a white silicon oxide layer on the surface;
step 2: preparation of coating slurries
Weighing 50-60 g of titanium oxide (TiO)2) And 40 to 50g of zirconium oxide (ZrO)2) Or Yttria Stabilized Zirconia (YSZ) ceramicsAdding ceramic powder into a zirconia ceramic ball milling tank with the volume of 500-1000 mL, adding 200-400 mL of grinding balls, 250-500 mL of purified water and 10-20 g of PVB adhesive into the zirconia ceramic ball milling tank, sealing and filling the mixture into a planetary ball mill, operating at 500RPM for 24 hours, and filtering to remove zirconium balls to form 250-500 mL of slurry with the solid content of 40%;
and step 3: preparation of the coating
Uniformly coating the slurry formed in the step 2 on the silicon oxide layer formed in the step 1 by adopting a brush coating mode, wherein the coating thickness is 100-150 mu m, and naturally airing for 4 hours or heating and drying for 2 hours at 150 ℃;
and 4, step 4: in-situ sintering of coatings
And (3) placing the silicon carbide (SiC) heating element coated with the coating formed in the step (3) into a high-temperature sintering furnace, heating to 1200-1400 ℃ at the heating rate of 10-15 ℃/min, and preserving heat for 1-2 hours to generate a Zirconium Titanium Silicate (ZTS) protective layer on the surface.
3. A method of preparing a high temperature resistant protective coating for a silicon carbide (SiC) heating element according to claim 2, wherein: in said step 2, zirconium oxide (ZrO)2) The purity is more than or equal to 99.5 percent.
4. A method of preparing a high temperature resistant protective coating for a silicon carbide (SiC) heating element according to claim 2, wherein: in the step 2, Y in the yttria-stabilized zirconia ceramic powder2O3The content is 3-5%.
5. A method of preparing a high temperature resistant protective coating for a silicon carbide (SiC) heating element according to claim 2, wherein: in the step 2, the ratio of the grinding balls is D10: D6: D4: 2:5: 3.
6. A method of preparing a high temperature resistant protective coating for a silicon carbide (SiC) heating element according to claim 2, wherein: in the step 2, the PVB content of the PVB adhesive is 3-6W%.
CN201910680290.1A 2019-07-26 2019-07-26 High-temperature-resistant protective coating of silicon carbide heating element and preparation method thereof Active CN112299883B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910680290.1A CN112299883B (en) 2019-07-26 2019-07-26 High-temperature-resistant protective coating of silicon carbide heating element and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910680290.1A CN112299883B (en) 2019-07-26 2019-07-26 High-temperature-resistant protective coating of silicon carbide heating element and preparation method thereof

Publications (2)

Publication Number Publication Date
CN112299883A true CN112299883A (en) 2021-02-02
CN112299883B CN112299883B (en) 2022-06-07

Family

ID=74329146

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910680290.1A Active CN112299883B (en) 2019-07-26 2019-07-26 High-temperature-resistant protective coating of silicon carbide heating element and preparation method thereof

Country Status (1)

Country Link
CN (1) CN112299883B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115385673A (en) * 2022-09-26 2022-11-25 武汉科技大学 High-strength silica brick for hydrogen metallurgy and preparation method thereof

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1260528A (en) * 1968-04-22 1972-01-19 Polaroid Corp Photographic diffusion transfer products and processes
US6517960B1 (en) * 1999-04-26 2003-02-11 General Electric Company Ceramic with zircon coating
CN1656041A (en) * 2002-05-23 2005-08-17 圣戈本陶瓷及塑料股份有限公司 Zircon/zirconia mix for refractory coatings and inks
US20070170502A1 (en) * 2003-03-24 2007-07-26 Tominaga Koji Semiconductor device and method for manufacturing the same
CN101333113A (en) * 2007-06-28 2008-12-31 科发伦材料株式会社 Material for baking multilayer ceramic capacitor, manufacturing method thereof and regenerating method
CN101555164A (en) * 2008-04-11 2009-10-14 中国科学院金属研究所 Preparation method of surface coating for enhancing high-temperature oxidation resistance of silicon carbide foam ceramic
CN102503581A (en) * 2011-09-22 2012-06-20 中南大学 Long-term high-temperature oxidation-resistant multi-element composite ceramic coating for carbon/carbon composite material and preparation and application methods thereof
CN103693936A (en) * 2013-12-13 2014-04-02 广西大学 Preparation method of nanopowder-based composite thermal insulation material
CN105948821A (en) * 2016-04-27 2016-09-21 航天材料及工艺研究所 Lightweight carbon fiber thermal insulation material surface pore-sealing method
CN107459369A (en) * 2017-09-07 2017-12-12 景德镇陶瓷大学 One kind prepares ZrSiO using non-hydrolytic sol-gel technique in SiC substrates4The method of film
CN107709273A (en) * 2015-10-27 2018-02-16 株式会社Inui Coating fluid, coating fluid composition and the refractory material with coating layer

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1260528A (en) * 1968-04-22 1972-01-19 Polaroid Corp Photographic diffusion transfer products and processes
US6517960B1 (en) * 1999-04-26 2003-02-11 General Electric Company Ceramic with zircon coating
CN1656041A (en) * 2002-05-23 2005-08-17 圣戈本陶瓷及塑料股份有限公司 Zircon/zirconia mix for refractory coatings and inks
US20070170502A1 (en) * 2003-03-24 2007-07-26 Tominaga Koji Semiconductor device and method for manufacturing the same
CN101333113A (en) * 2007-06-28 2008-12-31 科发伦材料株式会社 Material for baking multilayer ceramic capacitor, manufacturing method thereof and regenerating method
CN101555164A (en) * 2008-04-11 2009-10-14 中国科学院金属研究所 Preparation method of surface coating for enhancing high-temperature oxidation resistance of silicon carbide foam ceramic
CN102503581A (en) * 2011-09-22 2012-06-20 中南大学 Long-term high-temperature oxidation-resistant multi-element composite ceramic coating for carbon/carbon composite material and preparation and application methods thereof
CN103693936A (en) * 2013-12-13 2014-04-02 广西大学 Preparation method of nanopowder-based composite thermal insulation material
CN107709273A (en) * 2015-10-27 2018-02-16 株式会社Inui Coating fluid, coating fluid composition and the refractory material with coating layer
CN105948821A (en) * 2016-04-27 2016-09-21 航天材料及工艺研究所 Lightweight carbon fiber thermal insulation material surface pore-sealing method
CN107459369A (en) * 2017-09-07 2017-12-12 景德镇陶瓷大学 One kind prepares ZrSiO using non-hydrolytic sol-gel technique in SiC substrates4The method of film

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
AMIT KUMAR YADAV等: "Crystallization of ZrSiO4 from a SiO2−ZrO2 Binary System: The Concomitant Effects of Heat Treatment Temperature and TiO2 Additions", 《AMERICAN CHEMICAL SOCIETY》 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115385673A (en) * 2022-09-26 2022-11-25 武汉科技大学 High-strength silica brick for hydrogen metallurgy and preparation method thereof

Also Published As

Publication number Publication date
CN112299883B (en) 2022-06-07

Similar Documents

Publication Publication Date Title
CN107540400A (en) A kind of SiC with compound interfacef/ SiC ceramic based composites
CN109553430A (en) A kind of SiC with compound interfacef/ SiC ceramic based composites and preparation method thereof
CN108585897B (en) Refractory metal high-temperature oxidation-resistant Si-Mo-YSZ coating and preparation method thereof
CN102093083B (en) Preparation method for ablation-resistant coating made of carbon/carbon composite material HfC
CN113307660B (en) Self-healing environmental barrier coating for ceramic matrix composite and preparation method thereof
CN104356696B (en) A kind of method that rare earth silicate coating and C/SiC composite material surface prepare coating
Lu et al. Volatility diagram of ZrB2‐SiC‐ZrC system and experimental validation
CN114349502B (en) Titanium-doped lanthanum hafnate ceramic for low-thermal-expansion thermal/environmental barrier coating and preparation method thereof
CN111004990A (en) MAX phase coating for thermal barrier coating anti-melting CMAS corrosion and thermal spraying preparation method
CN113800955B (en) Multilayer ceramic matrix composite thermal protection coating and preparation method and application thereof
CN110981546A (en) Anti-oxidation ZrB on surface of C-C composite material2-SiC-Y2O3Coating and method for producing the same
CN112299883B (en) High-temperature-resistant protective coating of silicon carbide heating element and preparation method thereof
CN112279685A (en) MTaO with environmental thermal barrier coating4Graphite-based composite material and preparation method thereof
CN114988895A (en) Impact-resistant thermal cycle and CMAS corrosion resistant complex phase eutectoid environmental barrier coating and preparation method thereof
CN100532319C (en) Mo-corundum ceramic material and low-temperature sintering method
Yu et al. Nanosized (Zr, Hf) O2 coating reinforced by AlN whiskers for the ablation protection of SiC coated C/C composites
CN100509692C (en) Tungsten corundum ceramic material and low temperature sintering method
CN115572164A (en) High-toughness composite nano ceramic material and preparation method thereof
KR100520436B1 (en) Method for Making Oxidation Protective Double Coating for Carbon/Carbon Composite
KR102054373B1 (en) The Structure coated environmental barrier coating material and the method of coating the environmental barrier coating material
CN114368969A (en) TiSi2Gd-doped2Zr2O7Ceramic material, preparation method and thermal barrier coating
CN111410560A (en) Preparation method of silicified graphite with high-density SiC coating
Voronov et al. An Investigation of the Protective Action of a Coating Based on Yttrium Aluminosilicate System on Silicon Carbide Material at a Temperature up to 1500° С
CN117430405B (en) Antistatic ceramic tile and preparation method thereof
CN114892163B (en) High-temperature antioxidant protective coating material, preparation method and application

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant